OBJECT D, 58920 (Decayed)
Orbit data source: Space-Track
OBJECT D, 58920 was a satellite in LEO that was launched on Sat, 03 Feb 2024 UTC via a JIELONG-3 launch vehicle from the South China Sea Launch Area (SCSLA). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.
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58920 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Decayed Commercial Communications
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.6 m
Radar Cross Section
0.330 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 OBJECT D
1 58920U 24024D 25241.76751780 .11774272 24781-5 70736-3 0 9995
2 58920 97.3142 330.9371 0011286 286.1594 73.8464 16.40979217 88364Epoch: 2025-08-29T18:25Z
TLE epoch observation values (Epoch: 2025-08-29T18:25:13.537Z)
Latitude
-0.00002°
Longitude
76.41926°
Altitude
164.407 km
Speed
7.809 km/s
True Right ascension
22h 03m 44s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:30:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167.38 km
Perigee altitude
152.622 km
Semi-major axis
6,538.138 km
Eccentricity
0.00113
Inclination
97.3142°
RAAN
330.9371°
Arg. of periapsis
286.1594°
True anomaly
73.97067°
Mean anomaly
73.8464°
Eccentric anomaly
73.90853°
Mean motion
4.10546 °/min
Orbital period
87.69 mins
BSTAR
0.00070736
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Other satellites on launch #24 in the year 2024 (2024-02-03 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OBJECT D Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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